本研究主要是探討拍翼式微飛行器在拍動過程中,如何準確的得知機構運動相對於氣動力訊號之關
聯,拍翼機固定之夾治具係由放電線切割加工製作,另因考慮翅膀上下起始點位置,而設計計數器電
路搭配編碼齒輪達成精確的定位。控制程式使用美商國家儀器公司LabVIEW 軟體,搭配資料擷取器,
完成開發自動化的實驗設備,加上高速攝影機拍攝流場煙線圖並與量測訊號同步,紀錄拍翼特定位置
所產生的氣流走向。本研究所開發測試設備可減少因實驗步驟繁複及資料後處理分析的時間,並能拍
攝獲得拍翼拍動過程中周遭之渦流結構,證明本研究團隊發展之拍翼機能產生升推力之機制。 The purpose of this study is to investigate the flapping-MAY aerodynamics and focus on the body
movement relative to the signal of aerodynamic during flapping process. To fix the flapping-MAY at testing
section, the author has fabricated a fixture by wire electrical discharge machining. Another special device,
the counter circuit with a code and a position gear, was fabricated to get the precise attitude of the flapping
wing. The control program for starting and recording is edited by LabVIEW software. It is fit the data
acquisition device. So, the experimental setup is approaching automatic data acquisition and dealing the data
of aerodynamics. That means the setup is time economy compare to traditional process. From the results, we
can get the clear flow phenomena of lift and thrust-indicative vortices at the rear region of flapping wing.